Advanced Battery Technology
EMC Notebook

Shielding Theory (A Critical Look)

By George M. Kunkel
Spira Mfg. Corp

Introduction

During the late 60s and early 70s, I taught courses on EMC system design at the Extension Department of UCLA. One of the subjects covered was Shielding of EM Waves. The theory which was taught is consistent with the theory contained in the book by Ott. One of my students (who had a PhD degree in Physics from MIT) took exception to the theory. His comments were that the impedance of the barrier assumes an infinitely thick barrier where the thickness of the barriers on his spacecraft are of finite thickness, and absorption loss is an I2R loss, not skin effect. This paper will examine these comments and other comments which I encountered during my 17 years as chairman of the Technical Committee on Interference Control of the EMC Society of the IEEE.

Shielding Critique

Shielding theory stipulates that there is a reflection loss “R”, absorption loss “A” and a re-reflection coefficient “B” and that the energy in the wave emanating from the transmitted side of the barrier is equal to the energy striking the barrier minus the losses as a result of: (1) the reflection loss at the incident side of the barrier, (2) loss at the transmitted side of the barrier, and (3) the losses inside the barrier. The theory also stipulates that there is a re-reflection coefficient that exists when the barrier is less than the extension depth of the wave (i.e., when the thickness of the shielding barrier is less than 2P times the skin depth). The paragraphs that follow evaluate the shielding theory as presented by Ott. (Ott is used because the shielding theory presented in his book is the theory which is accepted by the EMC Society of the IEEE.)

Reflection Loss

The reflection loss as utilized in shielding theory is obtained directly from our textbooks on electromagnetic theory. However, the boundary conditions are not consistent with the boundary conditions used in the textbooks. The accepted equation of the reflection loss “R” is:


The boundary condition stipulated in the text books is that the thickness of the barrier is at least an extension depth or 2Pd In shielding theory there is no boundary condition (i.e., the impedance of the barrier is consistent irrespective of the thickness of the barrier). It can be shown that the actual impedance of the barrier varies significantly with the thickness of the barrier when the thickness is less than the extension depth. The equation for the impedance of the barrier can be obtained by integrating the thickness with respect to skin effect. That is, the normalized conductive area of a barrier is equal to:

for all thickness of a barrier. This yields an impedance of a barrier as follows:



As an example, we know from the ITT handbook that the area of a #10 copper wire conductor is 5.26 x 10-6 meters squared and it has a resistance of 3.27 x 10-3 ohms per meter length. If we take the wire and flatten it out to be a sheet one meter wide, the thickness would be 5.26 x 10-6 meters. The resistance would remain the same or 3.27 x 10-3 ohms per meter length. This can be verified by using the equation for the resistance of a metal sheet of equal length and width, i.e.,

The contents of the table below illustrate the significant difference in the value of the impedance as a function of the frequency of a wave striking the barrier and the Equations 4 and 6.

It is interesting to note that the thickness of the barrier is much less than the skin depth (as is the case for the frequency at 1kHz) the resistance associated with the impedance of ZB4 and ZB6 is the same as the resistance of the wire, i.e.,


It can also be noted that when the thickness is greater than the extension depth, the impedance is the same for ZB4 and ZB6 (as in the case for the frequency at 10GHz).

This difference in the impedance of the barrier means that there must be a correction factor to correct for the actual impedance when the thickness of the barrier is less than the extension depth. It is interesting to note that the value of the difference in the impedance between ZB4 and ZB6 is approximately equal to the value of the re-reflection coefficient “B” as defined by Ott, i.e.,


Absorption Loss

Ott, as well as all other books and papers on shielding, describe the skin effect as an absorption loss, i.e.,


We learn from high school physics classes that power (absorption ) loss is an I2R factor. Hallen tells us that the power (absorption) loss in a shielding barrier when the barrier is thicker than an extension depth is as follows:


The term “absorption less” used in the EMC community as illustrated by Ott is really an attenuating factor caused by skin effect, not as an absorption or power loss.

Re-Reflection Coefficient

Shielding theory as described by Ott states that there is a reflection loss at the incident side of a shielded barrier and another at the transmitting side. At the incident side, the E field is reflected (the H field actually doubles). At the transmitting side the H field is reflected, where the impedance of the transmitted wave which leaves the barrier is identical to the impedance of the incident wave which strikes the barrier. This is implied to be true irrespective of the impedance of the wave. This means that if you have a pair of wires as illustrated in Figure 1 on page 18. If the transmission line is carrying a 20kHz signal, the impedance of the wave leaving the barriers will be approximately 1.8 x 106 ohms, i.e


The wave emanating from the pair of wires approximates that of an electric dipole antenna. The impedance of a wave as a function of distance from an electric dipole antenna is approximated by Equation 9:

If the pair of wires is replaced by a transformer which is carrying 20kHz current, the impedance of the wave emanating from the barrier is approximately 0.8 ohms, i.e.,

The wave emanating from a transformer approximates that of a magnetic dipole antenna. The impedance of a wave as a function of distance from a magnetic dipole antenna is approximated by:

This requires an intelligence of the electrons in a shielding barrier that is hard to accept, i.e.,


Hallen tells us that the impedance of the wave in the barrier is equal to the impedance of the barrier. He also tells us that the surface current density “Js” is equal to the H field; therefore the E field is equal to the H field times the impedance of the barrier. What the shielding theory tells us is that the relative magnitude of the H reflected field at the transmitted secondary side is a function of the impedance of the wave at the incident side. It is difficult to accept that the electrons (represented by the surface current density Js) as they move through the barrier have the capability of remembering what the impedance of the forcing (or incident) field is and reacting at the secondary side in a relationship which is equal to the impedance of the wave at the incident side (i.e., the relative magnitude of the H field emanating from the transmitted side of the barrier is a function of the impedance of the incident wave).



EM Shielding Using Circuit Theory

The undergraduate courses on electromagnetic theory introduce the concept of an electromagnetic wave by driving a pair of parallel plates with an AC voltage source as illustrated in Figure 2.



As illustrated, a displacement field (displacement current) is generated between the plates. At the edge of the plates the lines of force bow out creating an EM field. If a shielding barrier is placed in the path of the lines of force of the field, the lines of force will cause a current Js to flow in the barrier as illustrated in Figure 3.

We know from Hallen that the magnitude of Js will be approximately equal to twice the value of the H field of the incident wave at the barrier. The current Js will create E and H fields inside the barrier. The E field is parallel to the flow of the current and equal to JSZB. The H field is at right angles to the current flow and equal in magnitude. The H field will generate a back emf forcing the magnitude of the current in the barrier to decrease with depth where the incremental amplitude of Js varies as illustrated in Figure 4. Since the E and H fields vary directly proportionally to Js, the incremental E and H fields will decrease with depth. The current in the barrier on the secondary side of the barrier will be equal to “Js” attenuated by skin effect, i.e.,

The values of the E and H vector fields at the transmitted side will also be equal to the E and H fields at the incident side of the barrer as attenuated by skin effect, i.e.,



The current Js will generate a field on the transmitted side, where it is hypothesized that the filed will be equal to Et and Ht.

Note: Shielding theory as described by Ott tells us that the current Js (i.e., the H field) will be reflected at the transmitted side of the barrier where the reflection coefficient will be equal to the E field reflection coefficient at the incident side. We are also told that the magnitude of the E field emanating from the barrier on the secondary side is equal to that obtained using Equation 12 or 14. It is very difficult to accept the theory that the current Js and H field is reduced without an equal reduction in the E field (i.e., E = HZB). It is also difficult to accept the reduction of the current without an outside force being exerted on the shield.

Summary

We are told that the theory on the shielding of electromagnetic waves is derived directly from our textbooks on EM theory. However, significant anomalies exist between the contents of the information in our textbooks and the information presented in our shielding theory. These anomalies are as follows:

1. In the development of the reflection coefficient our textbooks stipulate two boundary conditions which are not observed in our shielding theory. These are:

   a) The thickness of a barrier is equal to an extension depth or greater.

   b) Impedance of the incident wave is equal to 377ohms.

2. Absorption (or power) loss in our textbooks is defined as an I2R loss. Shielding theory defines skin effect as an absorption loss.

3. Shielding theory as described by Ott tells us that the reflection coefficient at the transmitting side of the barrier is an H field reflection coefficient (i.e., at the incident side of the barrier the E field is reflected and at the secondary or transmitted side the H field is reflected. This yields an equal magnitude of reflected E and H fields by the barrier).

Our textbooks (i.e., Hallen) inform us that the value of E in the barrier is equal to H ZB . This means that when the H field in the barrier is reduced due to the reflection at the secondary side, the E field is reduced proportionally.

4. Shielding theory as presented by Ott informs us that the wave takes on the impedance of the barrier upon entering the barrier and that the impedance of the barrier is constant irrespective of the thickness of the barrier (i.e., the impedance of the barrier is not reduced as a function of the thickness of the barrier when the thickness of the barrier is less than the extension depth). This implies that the impedance of a barrier as seen by the wave can be as much as two or three orders of magnitude less than the resistance of the barrier as measured by a resistance bridge.



Conclusion

The electrical/electronic design engineering community views the EMC discipline as a black magic art. This to a large degree is due to the fact that the EMC engineers use: (1) different logic in solving problems; (2) different equation s to explain their logic; and (3) a different vocabulary than the rest of the scientific community. The anomalies listed in this paper illustrate some of the problems inherent in the communication problems between the EMC engineer and the scientific community.

It is strongly recommended that the EMC engineering community evaluate the theory, equations and vocabulary used within the EMC discipline. The purpose would be to better communicate with the rest of the technical community. The result would place the EMC discipline on a much stronger technical plane and provide young graduate engineers an opportunity to enter the exiting and complex EMC design engineering discipline directly from college. They could then directly apply the information contained in their engineering courses to solve their EMC problems.

References

[1] Hallen, Erik, Electromagnetic Theory, John Wiley & Sons Inc., New York, 1962.

[2] Hayt, William H., Engineering Electromagnetics, McGraw-Hill Book Co., New York, 1958.

[3] Hershberger, “Introduction to Electromagnetic Theory”, Class notes, ENGR 117 A/B UCLA, 1961.

[4] I.T.T, Reference Data for Radio Engineers, Stanford Press, Inc., New York, 1956.

[5] Kunkel, George M., “Design of Transfer Impedance Test Fixture Accurate Through 10GHz,” IEEE 1990 International Symposium on EMC, Washington DC, August 1990.

[6] Ott, Henry W., Noise Reduction Techniques in Electronic Systems, John Wiley & Sons, New York, 1976.

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